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DC 2
DME 2
BATT
DC 2
IN
IRS 3 PWR A
IRS 3 PWR B
LIGHTNING SENSOR
MFD 1 CTLR
MFD 2 CTLR
IRS 3 FAN IN
IN
IN
IN
IN
DC 1
DC 1
DC ESS
DC 1
BATT
DC 2 IN
4/6
DC 1
CB − NAV SYSTEM 2/6
GPS 1
GPS 2
HUD
HUD CTL PANEL
FMS 3 CDU IN
IN
IN
IN
IN
DC 1
DC 1
DC 2
GPWS
DC 2
DC 2
IN
RAD ALT 2
STBY ADI
STBY ALT/ASI
TCAS
VOR/ILS 1
RAD ALT 1 IN
IN
IN
IN
IN
DC 1
DC 2
BATT
DC ESS
DC ESS
DC 2
CB − NAV SYSTEM
IN
5/6
DC 2
CB − NAV SYSTEM 3/6
IRS 1 PWR A
IRS 1 PWR B
IRS 2 PWR A
IRS 2 PWR B
IRS 1 FAN IN
IN
IN
IN
IN
DC ESS
DC ESS
BATT
IRS 2 FAN
DC 2
DC ESS
IN
VOR/ILS 3 (OPT)
WX RADAR
WX RADAR CTLR 1
WX RADAR CTLR 2
VOR/ILS 2 IN
IN
IN
IN
IN
DC ESS
DC 1
DC 1
DC 1
DC 1
CB − NAV SYSTEM 6/6
CB − NAV SYSTEM
GF1120_002
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
CIRCUIT BREAKER − SYSTEM 2/2
CIRCUIT BREAKER SYSTEM
HYD
ICE
IND/RECORD
LDG GEAR
LIGHTS
NAV
OIL
OXYGEN
THRUST REV
BRT
FLIGHT INSTRUMENTS
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
11−20−2
DESCRIPTION
General 09−10−1
Flight Compartment Fire Warning 09−10−2
Fire Detecting System 09−10−2
Wheel Well Overheat Warning 09−10−2
Fire Agent Discharge Indication 09−10−2
Smoke Detection 09−10−2
Portable Fire Extinguishers 09−10−2
System Overview Schematic 09−10−3
Fire Control Handles 09−10−4
Engine Fire Control Handle 09−10−5
APU Fire Control Handle 09−10−5
Synoptic Pages 09−10−6
Fire Extinguisher assembly 09−10−7
Fire Extinguisher Discharge Squibs 09−10−7
Fire Extinguisher Gauges 09−10−8
Fire Zone Discharge Schematic 09−10−8
FIDEEX Control Unit 09−10−9
Main Engine Fire Detection 09−10−10
Main Engine FIDEEX Control 09−10−11
Engine FIDEEX Control Schematic 09−10−12
APU Compartment Fire Detection 09−10−13
APU FIDEEX Control Schematic 09−10−14
APU FIDEEX/FADEC Interface 09−10−15
APU FIDEEX/FADEC Control Schematic 09−10−15
Main Wheel Well (MWW) Overheat Detection 09−10−16
Smoke Detection 09−10−17
Pilot Initiated Test 09−10−18
EICAS Messages 09−10−20
EMS CIRCUIT PROTECTION
CB − Fire System 09−20−1
FIRE PROTECTION
TABLE OF CONTENTS
CHAPTER 9
09−00−1
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
09−00−1
Page
TABLE OF CONTENTS
FIRE PROTECTION
TABLE OF CONTENTS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
09−00−2
THIS PAGE INTENTIONALLY LEFT BLANK
GENERAL
A Fire Detection and Extinguishing (FIDEEX) system with fault discrimination is installed with fire
detectors located in each engine nacelle and in the APU compartment.
The FIDEEX system interfaces with numerous airplane equipment and provides the following
capabilities:
· Monitor zones for fire/overheat/smoke events and FIDEEX system health and status.
· Automatic detection and reporting of fire events for each of the two power plants and the
Auxiliary Power Unit (APU).
· Fire extinguishing for each of the power plant and APU upon receipt of pilot initiated arming
and discharging commands.
· Automatic detection and reporting of overheat events for the two Main Wheel Wells (MWWs).
· Automatic detection and reporting of smoke events for each of the lavatories (fwd/aft),
baggage compartment, up to four cabin closets (requires installation of optional smoke
detectors) and avionics bay.
BAGGAGE COMPARTMENT
SMOKE DETECTION
(OPTIONAL)
MAIN LANDING GEAR
OVERHEAT DETECTION
APU FIRE DETECTION/
EXTINGUISHING SYSTEM
　
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